Raytheon 1900D

Service difficulty reports · 7,152

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '1900D'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA020510017Window · failed(CAN) ON CLIMB OUT THROUGH APPROXIMATELY 17,000 FT EXPERIENCED A LOUD BANG IN THE CABIN. REALIZING CABIN WAS DECOMPRESSED, THE CREW REQUESTED IMMEDIATE DESCENT. THE CREW DECIDED NOT TO DEPLOY PASSENGER MASKS SINCE THEY WERE AT A LOW ALTITUDE AND WOULD CAUSE MOApr 25, 2002 · Beech 1900D · Passenger Compartment WindowsSDR NSVA0210Wheel · separatedAIR DISPATCH RECEIVED A REPORT THAT AIRCRAFT HAD LOST THE NR 4 MAIN WHEEL ASSEMBLY DURING TAKEOFF. CREW CONTINUED TO IAD WHERE THE TOWER CONFIRMED THAT A WHEEL WAS MISSING. CREW DECLARED AN IN FLIGHT EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTEDApr 25, 2002 · N221CJ · Beech 1900D · Wheel/Ski/FloatSDR CA020424001Gyro · malfunctioned(CAN) ON DEPARTURE GOT YELLOW HEADING FLAG, WHICH WAS CLEARED, HAPPENED AGAIN AT TOC, CLEARED. IN CRUISE GOT RED HEADING ON NR 1 SYSTEM, SWITCHED TO HDG ALL ON NR 2 REVERSION PANEL. RETURNED TO YYC. MAINTENANCE REPLACED THE NR 1 DIRECTIONAL GYRO, TESTEDApr 23, 2002 · Beech 1900D · Directional Gyro and Indicating SystemSDR GLBA2002055Flow Divider · leakingFUEL ODOR IN COCKPIT ON TAXI, INSPECTED FOUND RIGHT FUEL FLOW DIVIDER LEAKING, REPLACED OPS CHECKED SYSTEM SATISFACTORYApr 20, 2002 · N251GL · Beech 1900D · Aircraft Fuel SystemSDR S2YA02015Engine · making metalFLT 1270 - MKE-CMH - THE LEFT OIL PRESSURE ILLUMINATED IN FLIGHT. THE CREW MADE AN UNEVENTFUL LANDING. OUT STATION MAINTENANCE SERVICED THE LEFT ENGINE WITH OIL AND THE CREW DID A GROUND RUN. AFTER SHUTDOWN OF THE GROUND RUN, THERE WAS FLAMES COMING OUT OF Apr 17, 2002 · N881SK · Beech 1900D · Engine (Turbine/Turboprop)SDR CA020417001Windshield · cracked(CAN) DURING CLIMBOUT FROM YYC THE CO PLIOTS WINDSHIELD CRACKED. AIRCRAFT WAS LEVELED OFF AND RETURNED TO AIRPORT. THE OUTER PLY OF WINDSHIELD WAS CRACKED WITH NO APPARENT REASON SUCH AS IMPACT. THE WINDSHIELD WAS REPLACED AND THE OLD SENT FOR INVESTIGATION.Apr 15, 2002 · Beech 1900D · Flight Compartment WindowsSDR GLBA2002052Tach Generator · intermittentLEFT N1 FLUXUATION, REPLACED TAC GEN OPS CHECKED SATISFACTORYApr 15, 2002 · N249GL · Beech 1900D · Engine Indicating SystemSDR GUU2002F00003Computer · malfunctionedDURING TAKE OFF STALL WARNING WENT OFF. REMOVED AND REPLACED STALL WARNING COMPUTER, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.Apr 14, 2002 · N38537 · Beech 1900D · Stall Warning SystemSDR GLBA2002051Altimeter · failedCAPTAINS ALTIMETER FLAGGED. REPLACED, OPS CHECKED SATISFACTORY.Apr 14, 2002 · N219GL · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2002050Altimeter · inoperativeNR 1 ALTIMETER FAILED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY.Apr 13, 2002 · N150GL · Beech 1900D · Altimeter, Barometric/EncoderSDR GUU2002F00001Bolt · looseAT SCHEDULED ROUTINE INSPECTION VERTICAL FIN LOWER ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.Apr 12, 2002 · N49543 · Beech 1900D · FastenersSDR CA020422004Keel · worn(CAN) DURING INVESTIGATION OF A DC LOAD SHARE PROBLEM BETWEEN BOTH GENERATOR FOUND FOUR WIRES CHAFFED IN THE LT NACELLE ON THE OUTBOARD KEEL WEB ASSY. THE DAMMAGE ON THE KEEL WEB WAS DUE TO ELECTRICAL ARCING BETWEEN THE WIRE AND THE KEEL WEB ASSY. NO PROTECTIOApr 11, 2002 · Beech 1900D · Fuselage Main, KeelSDR GLBA2002048Sensor · failedLEFT & RIGHT ENVIRONMENTAL FAILURE. REPLACED TEMP SENSOR.Apr 11, 2002 · N151GL · Beech 1900D · Cabin Cooling SystemSDR GLBA2002049Converter · failedRIGHT WINDSHIELD WIPER FAILED. REPLACED CONVERTER, OPS CHECKED SATISFACTORY.Apr 11, 2002 · N151GL · Beech 1900D · Windshield/Door Rain/Ice RemovalSDR CA020515014Rivet · sheared(CAN) UPON INVESTIGATION OF A FUEL LEAK LT AUXILIARY FUEL TANK, "PRC" REMOVED AND FOUND 6 RIVET HEADS ATTACHED TO THE "PRC", AT LT KEEL RIB INSTALLATION BL.91.75. SHANK'S REMOVED AND NEW RIVETS INSTALLED.Apr 7, 2002 · Beech 1900D · Fuel StorageSDR GLBA2002047Altimeter · inaccurateCAPTAINS ALTIMETER INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORYApr 7, 2002 · N100UX · Beech 1900D · Navigation SystemSDR GLBA2002046Warning System · malfunctionedRIGHT ENVIRONMENTAL FAIL ILLUMINATED. COULD NOT DUPLICATE FAULT.Apr 6, 2002 · N150GL · Beech 1900D · Cabin Cooling SystemSDR GLBA2002045Altimeter · inaccurateCAPTAINS ALTIMETER ALTITUDE INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORYApr 6, 2002 · N202GL · Beech 1900D · Navigation SystemSDR CA020419003Relay · corroded(CAN) DURING PREFLIGHT CHECK PILOT PULLED THE FIRE HANDLE TO CHECK THE FUEL SHUTOFF VALVE OPERATION, WHEN HE PUSH IT BACK THE VALVE STAYED CLOSED.AFTER INVESTIGATION WE FOUND ALL THE CONTACT ON RELAY (A236K1)CORRODED AND FEW PIN BROKEN. RELAY AND WIRE WAS REPApr 4, 2002 · Beech 1900D · Engine Emergency Shutdown SystemSDR CA020506004Socket · cracked(CAN) DURING A ROUTINE INSPECTION A CRACK WAS NOTED IN THE AREA OF THE MAIN LANDING GEAR LOWER TORQUE KNEE LUGS.THE PISTON AND AXLE ASSY WAS REPLACED.THE CRACKED AXLE AND PISTON ASSY WERE SENT FOR O/H.THE SOCKET ASSY WAS REPLACED AT THE OVERHAUL FACILITY (CRACApr 3, 2002 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2002044Indicator · failedRIGHT ITT INDICATOR FAILED ON CLIMBOUT. REPLACED INDICATOR.Apr 2, 2002 · N179GL · Beech 1900D · Engine EGT/TIT Indicating SystemSDR 2002FA0000549Keelbeam · crackedSMALL CRACK FOUND ON RIGHT HAND FORWARD OUTBOARD WHEEL WELL KEEL AT UPPER GEAR FENDER SUPPORT ANGLE (SUPPORT ANGLE IS PART OF KEEL CASTING).Mar 29, 2002 · N61HA · Beech 1900D · Fuselage Main, KeelSDR B2P2002F00002Screw · brokenCUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKAGE FROM BLADE SOCKETS. PROPELLER WAS DISASSEMBLED AND INSPECTED. UPON FURTHER INVESTIGATION, THE PRELOAD PLATE SCREWS WERE SEVERELY WORN AND ONE WAS BROKEN IN TWO PIECES. LOMar 29, 2002 · N48544 · Beech 1900D · Propeller Hub SectionSDR B2P2002F00001Bearing Race · brokenCUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKING FROM BLADE SOCKETS. UPON DISASSEMBLY IT WAS NOTED THAT THE BEARING RACES ON BLADES (SN 2579 AND 2583 HAD FAILED COMPLETELY AND WERE IN MANY PIECES. POSSIBLE CAUSE COULD BEMar 29, 2002 · N48544 · Beech 1900D · Propeller Hub SectionSDR B2P2002F00000Bearing Race · brokenCUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKING FROM BLADE SOCKETS. UPON DISASSEMBLY, IT WAS NOTED THAT THE BEARING RACES ON BLADES (SN 2579 AND 2583) HAD FAILED COMPLETELY AND WERE IN MANY PIECES. POSSIBLE CAUSE COULD Mar 29, 2002 · N48544 · Beech 1900D · Propeller Spinner SectionSDR GLBA2002043Switch · inoperativeLEFT PUSH TO-TALK SWITCH FAILED REPLACED OPS CHECKED SATISFACTORYMar 29, 2002 · N170GL · Beech 1900D · Communications SystemSDR CA020405003Line · chafed(CAN) THE L/H FUEL CROSS TRANSFER TUBE WAS FOUND CHAFED THROUGH AND SEEPING FUEL. THE WEAR MARK ON THE TUBE MEASURED APPROXIMATELY 5/16 INCH IN LENGTH X 1/8 INCH IN WIDTH. REF: IPC 28-20-00. WEAR OCCURRED FROM THE WIRE BUNDLE COVERING OF THE GEAR UPLOCK MICROSMar 27, 2002 · Beech 1900D · Aircraft Fuel Distribution SystemSDR JJB2002F00000Link · dischargedDURING ROUTINE INSPECTION, FOUND LEFT ENGINE ANTI-ICE VANE DOOR SHOCK LINKS MISSING PARTS AND DOOR DISCONNECTED. NOTE: DOWEL PINS FELL OUTOF SPRING RETAINER.Mar 22, 2002 · N835CA · Beech 1900D · Air Intake Anti/De-Ice SystemSDR CA020419002Relay · corroded(CAN) DURING PREFLIGHT CHECK PILOT PULLED THE LT FIRE HANDLE TO CHECK THE SHUTTOFF VALVE OPERATION, WHEN HE PUSH BACK THE HANDLE THE VALVE STAYED CLOSED. SEVERAL TRIES WERE NECESSARY TO OPEN THE VALVE. DURING TROUBLESHOOTING, THE PROBLEM DID NOT REOCCUR BUT AFMar 21, 2002 · Beech 1900D · Engine Emergency Shutdown SystemSDR GLBA2002039Warning System · malfunctionedOVER FLEW MCK, BATT-TIE ANNUN, OPENED IN FLIGHT, WOULD NOT RESET. PERFORMED SELF TEST SEVERAL TIMES, NO FAULT FOUND. INSPECTED AND CHECKED OKAY FOR SERVICE.Mar 19, 2002 · N249GL · Beech 1900D · DC Indicating SystemSDR GLBA2002037Encoder · inaccurate#2 ENCODER REPORTED HIGH BY ATC, REPLACED ENCODING ALTIMETER OPS CHECKED SYSTEM SATISFACTORYMar 18, 2002 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2002038Altimeter · malfunctionedALTIMETER SPLIT. COULD NOT DUPLICATE, OPS CHECKED SATISFACTORY.Mar 18, 2002 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2002036Wire · brokenOIL TEMP INDICATOR FAILED. REPAIRED BROKEN WIRE, OPS CHECKED SYSTEM SATISFACTORY.Mar 18, 2002 · N255GL · Beech 1900D · Engine Oil System WiringSDR GLBA2002034Motor · inoperativeLANDING GEAR RELAY C/B POPPED, REPLACED HYDRAULIC MOTOR OPS CHECKED SYSTEM SATISFACTORYMar 16, 2002 · N100UX · Beech 1900D · Main Landing Gear Strut/Axle/TruckSDR GLBA2002032Valve · leakingLEFT AND RIGHT ENVIROMENTAL FAILURE AND LOSS OF PRESSURIZATION, REPLACED INSTRUMENT AIR VALVEMar 13, 2002 · N151GL · Beech 1900D · Air Distribution SystemSDR GLBA2002033Torque Link · damagedLEFT MAIN TORQUE KNEE SEPARATED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY.Mar 13, 2002 · N170GL · Beech 1900D · Main Landing Gear Strut/Axle/TruckSDR GLBA2002035A/C Pack · failedLEFT ENVIRONMENTAL FAILURE ON T/O.Mar 12, 2002 · N226GL · Beech 1900D · Cabin Cooling SystemSDR GLBA2002031Transmitter · intermittentRT TORQUE INDICATOR FAILED, REPLACED TRANSMITTER OPS CHECKED SYSTEM SATISFACTORYMar 10, 2002 · N247GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR CA020307003Bracket · cracked(CAN) CREW BEGAN TAXI FROM OUTSTATION&NOTED THAT "GREEN" NOSEGEAR IND. EXTINGUISHED&"RED" UNSAFE IND. ILLUMINATED. A/C SHUTDOWN, PAX DEPLANED&A/C CHOCKED. MAINT FOUND BRACKET THAT PROVIDES DO WN MICRO SWITCH STRIKE PLATE HAD CRACKED ACROSS ATTACHMENT FLANGE&WOMar 7, 2002 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2002030Switch · out of adjustFLAPS STUCK AT 17 PERCENT, ADJUSTED FLAP SAFTEY SWITCH OPS CHECKED SYSTEM SATISFACTORYMar 4, 2002 · N208GL · Beech 1900D · Trailing Edge Flap Control SystemSDR GLBA2002029Connector · looseLEFT GENERATOR TIE ILLUMINATED ON T/O, RESECURED CONNECTOR PLUG & PCB OPS CHECKED SYSTEM SATISFACTORYMar 2, 2002 · N245GL · Beech 1900D · AC Generation SystemSDR GLBA2002027Motor · failedFLAPS STUCK AT 17 PERCENT.Mar 2, 2002 · N169GL · Beech 1900D · Trailing Edge Flap ActuatorSDR GLBA2002028Tach Generator · fluctuatesLEFT N1 INDICATOR FLUCTUATING. REPLACED TACH GEN, OPS CHECKED SYSTEM SATISFACTORY.Mar 2, 2002 · N204GL · Beech 1900D · Engine RPM Indicating SystemSDR GLBA2002026Warning System · malfunctionedLEFT GEN TIE ANNUNCIATOR ILLUMINATED IN-FLIGHT. COULD NOT DUPLICATE.Mar 1, 2002 · N245GL · Beech 1900D · DC Power Distribution SystemSDR CA020227005Actuator · inoperative(CAN) DURING NORMAL APPRAOCH, CREW EXTENDED LANDING GEAR BUT DID NOT GET A NOSE GREEN. GEAR WAS CYCLED WITHOUT CHANGE. EMERGENCY PROCEDURES PROVIDED FOR MANUAL EXTENSION BUT STILL WITHOUT GREEN. DUE TO SYSTEM WIRING, THE GEAR WAS ASSERTAINED DOWN DUE TO THE ABFeb 27, 2002 · Beech 1900D · Landing Gear ActuatorSDR AMW2002F00001Hose · leakingENROUTE, THE CREW NOTICED THAT THE OIL PRESSURE LOW LIGHT FLICKERED AND THE OIL PRESSURE INDICATED LOW. THE CREW REDUCED POWER ON THE LEFT ENGINE AND LANDED WITHOUT INCIDENT.Feb 27, 2002 · N163YV · Beech 1900D · Engine Oil Distribution (Airframe Furnished)SDR CA020225001Bearing · corroded(CAN) R/H AILERON FOUND WITH EXSCESSIVE UP AND DOWN PLAY.PLAY WAS CAUSED DUE TO R/H AILERON TERMINAL BELLCRANK BEARING WORN.BALL INSIDE BEARING WAS FOUND HEAVILY CORRODED AND OUT OF SHAPE.Feb 25, 2002 · Beech 1900D · Aileron Control SystemSDR 2002F00272Door · out of rigDURING CREW CHANGE, THE ON COMING CREW FOR AIRCRAFT FOUND THE RIGHT FORWARD EMERGENCY EXIT DOOR NOT FLUSH WITH THE EXTERIOR OF THE AIRCRAFT. AIRCRAFT MAINTENANCE FOUND THE DOOR TO BE OUT OF RIG, AND ADJUSTED THE DOOR PER MAINTENANCE INSTRUCTION. RETURNED TO Feb 25, 2002 · N237YV · Beech 1900D · Emergency ExitsSDR CA020411009Wire · chafed(CAN) AFTER DEPARTURE, CREW NOTICED FAINT ODOUR AND SAW AUTOFEATHER CB WAS POPPED. ELECTED TO RETURN AND DURING DECENT ODOUR INCREASED ACCOMPANIED BY SMOKE. DEPLOYED AND DONNED O2 MASKS. WENT THRU EMERGENCY PROC: SMOKE DISSIPATED, UNEVENTFULL LANDING. DURINGFeb 24, 2002 · Beech 1900D · Propeller/Propulsor System WiringSDR CA020227007Wire · shorted(CAN) DURING CRUISE FLT, CREW NOTICED FAINT SMOKE SMELL, & NOTICED THAT PROP AUTOFEATHER CIRCUIT BREAKER HAD POPPED. THEY DECIDED TO RETURN TO YYC. DURING APPROACH / LDG PHASE OF FLT, SMELL OF SMOKE BECAME MORE NOTICEABLE. THE LDG & TAXIING TO GATE WENT UNEVEFeb 24, 2002 · Beech 1900D · Propeller/Propulsor System Wiring
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